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 26037.75300603 +.00000000 +00000-0 +19983-3 0 00000
2 23908 63.3200 172.7992 0844857 47.4453 319.4810 13.45804113 04
| Epoch (UTC): | 06 February 2026 18:04:19 |
| Eccentricity: | 0.0844857 |
| inclination: | 63.3200° |
| perigee height: | 457 km |
| apogee height: | 1718 km |
| right ascension of ascending node: | 172.7992° |
| argument of perigee: | 47.4453° |
| revolutions per day: | 13.45804113 |
| mean anomaly at epoch: | 319.4810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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