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 21398U 91039B 25346.14335332 .00000605 00000-0 73470-4 0 9995
2 21398 82.5224 218.2306 0022230 93.6672 266.7085 14.81747868841430
| Epoch (UTC): | 12 December 2025 03:26:25 |
| Eccentricity: | 0.0022230 |
| inclination: | 82.5224° |
| perigee height: | 608 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 218.2306° |
| argument of perigee: | 93.6672° |
| revolutions per day: | 14.81747868 |
| mean anomaly at epoch: | 266.7085° |
| orbit number at epoch: | 84143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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