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 08846U 76043B 22143.87348279 -.00000110 00000-0 -70903-4 0 9993
2 08846 81.2237 358.5918 0037465 334.1081 25.8213 14.08627448364418
| Epoch (UTC): | 23 May 2022 20:57:48 |
| Eccentricity: | 0.0037465 |
| inclination: | 81.2237° |
| perigee height: | 837 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 358.5918° |
| argument of perigee: | 334.1081° |
| revolutions per day: | 14.08627448 |
| mean anomaly at epoch: | 25.8213° |
| orbit number at epoch: | 36441 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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