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 data is extracted from the following two-line orbital elements,
1 21805U 91080B 25348.70334270 -.00000132 00000-0 00000-0 0 9999
2 21805 14.1033 346.8242 0001326 103.2314 254.7888 0.99189599 23876
| Epoch (UTC): | 14 December 2025 16:52:48 |
| Eccentricity: | 0.0001326 |
| inclination: | 14.1033° |
| perigee height: | 36087 km |
| apogee height: | 36098 km |
| right ascension of ascending node: | 346.8242° |
| argument of perigee: | 103.2314° |
| revolutions per day: | 0.99189599 |
| mean anomaly at epoch: | 254.7888° |
| orbit number at epoch: | 2387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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