Research any topic before you write.
Find related topics. | Discover entities. | See connections. | Build a topical map.
Orbiting Vehicle 1-8 (also known as OV1-8, OV1-8P,PasComSat,: 419 and Gridsphere), launched 14 July 1966, was the seventh satellite launched (fourth successfully) in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-8 was designed to test the passive communications utility of an aluminum grid sphere versus a balloon satellite…
History, Legacy & Measurement
Explore the main themes, entities and connections around OV1-8. Start with the topic map, then use the sections below for research and deeper semantic analysis.
Start with a few of the strongest sections from the source topic. These are research directions, not a list of keywords you must use.
High-confidence facts extracted from structured source data. Use them as anchors for further research.
Browse the full topic structure. Each item opens a new analysis centered on that subject.
Deeper signals for content research, entity SEO and topical coverage. The plain-language headings explain what each technical view is useful for.
See the strongest relationship patterns around the current topic before diving into the raw triples.
Use these terms to understand the vocabulary surrounding the topic, not as a checklist for keyword stuffing.
satellite ov1 satellites launched grid atlas program balloon orbit test rocket would series air aluminum lb mission 1966 launch experiments
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| OV1-8 | Apogee altitude | 1,013.00 km (629.45 mi) | 1.00 | infobox |
| OV1-8 | BOL mass | 3.2 kilograms (7.1 lb) | 1.00 | infobox |
| OV1-8 | COSPAR ID | 1966-063A | 1.00 | infobox |
| OV1-8 | Decay date | 4 January 1978 | 1.00 | infobox |
| OV1-8 | Dimensions | 9.1-meter (30 ft) sphere | 1.00 | infobox |
| OV1-8 | Eccentricity | 0.00102 | 1.00 | infobox |
| OV1-8 | Epoch | 14 July 1966 02:09:00 | 1.00 | infobox |
| OV1-8 | Inclination | 144.200° | 1.00 | infobox |
| OV1-8 | Launch date | 14 July 1966 02:10:02 (1966-07-14UTC02:10:02) UTC | 1.00 | infobox |
| OV1-8 | Launch mass | 10.4 kg (23 lb) with onboard rocket. | 1.00 | infobox |
| OV1-8 | Launch site | Vandenberg 576-B-3 | 1.00 | infobox |
| OV1-8 | Manufacturer | General Dynamics | 1.00 | infobox |
| OV1-8 | Mission type | Earth science | 1.00 | infobox |
| OV1-8 | Operator | USAF | 1.00 | infobox |
| OV1-8 | Perigee altitude | 998.00 km (620.13 mi) | 1.00 | infobox |
| OV1-8 | Period | 105.20 minutes | 1.00 | infobox |
| OV1-8 | Regime | Medium Earth Orbit | 1.00 | infobox |
| OV1-8 | Rocket | Atlas D | 1.00 | infobox |
| OV1-8 | SATCAT no. | S02324 | 1.00 | infobox |
These clusters group vocabulary that occurs around closely connected concepts in the source material.
Bridges can reveal useful research angles that are easy to miss in a flat list of related terms.