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 26100.05046168 +.00000000 +00000-0 +74121-4 0 00006
2 10121 74.0480 343.9871 0019473 260.6392 99.2560 14.37377489 01
| Epoch (UTC): | 10 April 2026 01:12:39 |
| Eccentricity: | 0.0019473 |
| inclination: | 74.0480° |
| perigee height: | 753 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 343.9871° |
| argument of perigee: | 260.6392° |
| revolutions per day: | 14.37377489 |
| mean anomaly at epoch: | 99.2560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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