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 26146.27329014 +.00000000 +00000-0 +14232-3 0 00000
2 23893 63.3194 249.4489 0850006 48.8417 318.2840 13.46178914 04
| Epoch (UTC): | 26 May 2026 06:33:32 |
| Eccentricity: | 0.0850006 |
| inclination: | 63.3194° |
| perigee height: | 452 km |
| apogee height: | 1721 km |
| right ascension of ascending node: | 249.4489° |
| argument of perigee: | 48.8417° |
| revolutions per day: | 13.46178914 |
| mean anomaly at epoch: | 318.2840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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