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 23908U 26103.95324198 +.00000000 +00000-0 +24091-3 0 00007
2 23908 63.3229 359.6791 0848262 48.4932 318.5793 13.46074629 07
| Epoch (UTC): | 13 April 2026 22:52:40 |
| Eccentricity: | 0.0848262 |
| inclination: | 63.3229° |
| perigee height: | 454 km |
| apogee height: | 1720 km |
| right ascension of ascending node: | 359.6791° |
| argument of perigee: | 48.4932° |
| revolutions per day: | 13.46074629 |
| mean anomaly at epoch: | 318.5793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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