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 25397U 98043D 22135.82047017 .00000071 00000-0 50934-4 0 9995
2 25397 98.8156 86.2064 0001264 151.1736 208.9513 14.23750758238786
| Epoch (UTC): | 15 May 2022 19:41:28 |
| Eccentricity: | 0.0001264 |
| inclination: | 98.8156° |
| perigee height: | 812 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 86.2064° |
| argument of perigee: | 151.1736° |
| revolutions per day: | 14.23750758 |
| mean anomaly at epoch: | 208.9513° |
| orbit number at epoch: | 23878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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