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 23608U 26042.19829086 +.00000000 +00000-0 +86018-3 0 00005
2 23608 98.2894 242.6614 0007519 124.1107 236.0854 15.45081666 04
| Epoch (UTC): | 11 February 2026 04:45:32 |
| Eccentricity: | 0.0007519 |
| inclination: | 98.2894° |
| perigee height: | 426 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 242.6614° |
| argument of perigee: | 124.1107° |
| revolutions per day: | 15.45081666 |
| mean anomaly at epoch: | 236.0854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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