View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 07735U 26069.47977093 +.00000000 +00000-0 +11377-3 0 00006
2 07735 114.9734 19.5036 0054294 284.7944 74.7127 14.25569452 00
| Epoch (UTC): | 10 March 2026 11:30:52 |
| Eccentricity: | 0.0054294 |
| inclination: | 114.9734° |
| perigee height: | 768 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 19.5036° |
| argument of perigee: | 284.7944° |
| revolutions per day: | 14.25569452 |
| mean anomaly at epoch: | 74.7127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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