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 26073.61875576 +.00000000 +00000-0 +10752-3 0 00006
2 07735 114.9738 30.9769 0054340 283.7565 75.7473 14.25571681 06
| Epoch (UTC): | 14 March 2026 14:51:00 |
| Eccentricity: | 0.0054340 |
| inclination: | 114.9738° |
| perigee height: | 768 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 30.9769° |
| argument of perigee: | 283.7565° |
| revolutions per day: | 14.25571681 |
| mean anomaly at epoch: | 75.7473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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