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 12771U 26100.98501956 +.00000000 +00000-0 +89102-3 0 00006
2 12771 82.8707 176.8525 0146793 336.0201 206.6203 13.68911357 04
| Epoch (UTC): | 10 April 2026 23:38:25 |
| Eccentricity: | 0.0146793 |
| inclination: | 82.8707° |
| perigee height: | 895 km |
| apogee height: | 1112 km |
| right ascension of ascending node: | 176.8525° |
| argument of perigee: | 336.0201° |
| revolutions per day: | 13.68911357 |
| mean anomaly at epoch: | 206.6203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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