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 data is extracted from the following two-line orbital elements,
1 15876U 85056B 23033.60089260 .00000056 00000-0 27190-3 0 9996
2 15876 8.6273 238.0627 6219200 326.2353 6.4231 3.53571818141820
| Epoch (UTC): | 02 February 2023 14:25:17 |
| Eccentricity: | 0.6219200 |
| inclination: | 8.6273° |
| perigee height: | 503 km |
| apogee height: | 23141 km |
| right ascension of ascending node: | 238.0627° |
| argument of perigee: | 326.2353° |
| revolutions per day: | 3.53571818 |
| mean anomaly at epoch: | 6.4231° |
| orbit number at epoch: | 14182 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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