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 10875U 26071.84576434 +.00000000 +00000-0 +50981-3 0 00007
2 10875 101.9697 26.9226 0033199 52.5701 336.1103 12.47071918 05
| Epoch (UTC): | 12 March 2026 20:17:54 |
| Eccentricity: | 0.0033199 |
| inclination: | 101.9697° |
| perigee height: | 1451 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 26.9226° |
| argument of perigee: | 52.5701° |
| revolutions per day: | 12.47071918 |
| mean anomaly at epoch: | 336.1103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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