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 24213U 26088.08422767 +.00000000 +00000-0 +96522-3 0 00002
2 24213 81.4617 220.3591 0512487 285.1102 69.3929 13.96966490 00
| Epoch (UTC): | 29 March 2026 02:01:17 |
| Eccentricity: | 0.0512487 |
| inclination: | 81.4617° |
| perigee height: | 531 km |
| apogee height: | 1278 km |
| right ascension of ascending node: | 220.3591° |
| argument of perigee: | 285.1102° |
| revolutions per day: | 13.96966490 |
| mean anomaly at epoch: | 69.3929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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