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 24797U 26020.24747242 +.00000000 +00000-0 +22805-3 0 00004
2 24797 86.8935 282.0276 0212739 276.2506 196.8156 14.47735758 06
| Epoch (UTC): | 20 January 2026 05:56:21 |
| Eccentricity: | 0.0212739 |
| inclination: | 86.8935° |
| perigee height: | 582 km |
| apogee height: | 884 km |
| right ascension of ascending node: | 282.0276° |
| argument of perigee: | 276.2506° |
| revolutions per day: | 14.47735758 |
| mean anomaly at epoch: | 196.8156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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