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 12758U 26073.26763064 +.00000000 +00000-0 +55715-3 0 00004
2 12758 82.8649 158.1465 0059056 110.2614 305.2309 13.82198666 04
| Epoch (UTC): | 14 March 2026 06:25:23 |
| Eccentricity: | 0.0059056 |
| inclination: | 82.8649° |
| perigee height: | 913 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 158.1465° |
| argument of perigee: | 110.2614° |
| revolutions per day: | 13.82198666 |
| mean anomaly at epoch: | 305.2309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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