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 23893U 26145.38188061 +.00000000 +00000-0 +12487-3 0 00006
2 23893 63.3195 251.7813 0849959 48.8289 318.2950 13.46176845 07
| Epoch (UTC): | 25 May 2026 09:09:54 |
| Eccentricity: | 0.0849959 |
| inclination: | 63.3195° |
| perigee height: | 452 km |
| apogee height: | 1721 km |
| right ascension of ascending node: | 251.7813° |
| argument of perigee: | 48.8289° |
| revolutions per day: | 13.46176845 |
| mean anomaly at epoch: | 318.2950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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