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 26065.34077948 +.00000000 +00000-0 +12606-3 0 00004
2 07735 114.9732 8.0307 0054237 285.8413 73.6694 14.25567170 04
| Epoch (UTC): | 06 March 2026 08:10:43 |
| Eccentricity: | 0.0054237 |
| inclination: | 114.9732° |
| perigee height: | 768 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 8.0307° |
| argument of perigee: | 285.8413° |
| revolutions per day: | 14.25567170 |
| mean anomaly at epoch: | 73.6694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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