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 23751U 26040.93480010 +.00000000 +00000-0 +70223-4 0 00006
2 23751 99.0302 56.7213 0000986 83.3969 276.7320 14.23532236 06
| Epoch (UTC): | 09 February 2026 22:26:06 |
| Eccentricity: | 0.0000986 |
| inclination: | 99.0302° |
| perigee height: | 813 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 56.7213° |
| argument of perigee: | 83.3969° |
| revolutions per day: | 14.23532236 |
| mean anomaly at epoch: | 276.7320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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