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 23802U 26128.75546514 +.00000000 +00000-0 +00000-0 0 00004
2 23802 79.8139 227.5104 6431120 210.4347 87.4541 1.29845949 03
| Epoch (UTC): | 08 May 2026 18:07:52 |
| Eccentricity: | 0.6431120 |
| inclination: | 79.8139° |
| perigee height: | 6288 km |
| apogee height: | 51937 km |
| right ascension of ascending node: | 227.5104° |
| argument of perigee: | 210.4347° |
| revolutions per day: | 1.29845949 |
| mean anomaly at epoch: | 87.4541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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