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 26021.50357905 +.00000000 +00000-0 +28476-3 0 00007
2 24797 86.8933 281.5643 0212709 271.9981 263.5098 14.47740657 03
| Epoch (UTC): | 21 January 2026 12:05:09 |
| Eccentricity: | 0.0212709 |
| inclination: | 86.8933° |
| perigee height: | 582 km |
| apogee height: | 884 km |
| right ascension of ascending node: | 281.5643° |
| argument of perigee: | 271.9981° |
| revolutions per day: | 14.47740657 |
| mean anomaly at epoch: | 263.5098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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