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 10121U 26040.61203550 +.00000000 +00000-0 +92026-4 0 00005
2 10121 74.0448 93.2791 0017983 20.5068 339.6803 14.37339023 01
| Epoch (UTC): | 09 February 2026 14:41:19 |
| Eccentricity: | 0.0017983 |
| inclination: | 74.0448° |
| perigee height: | 754 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 93.2791° |
| argument of perigee: | 20.5068° |
| revolutions per day: | 14.37339023 |
| mean anomaly at epoch: | 339.6803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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