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 22138.49098164 .00000128 00000-0 75898-4 0 9999
2 25397 98.8158 88.8830 0001402 146.5698 213.5569 14.23751696239164
| Epoch (UTC): | 18 May 2022 11:47:00 |
| Eccentricity: | 0.0001402 |
| inclination: | 98.8158° |
| perigee height: | 811 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 88.8830° |
| argument of perigee: | 146.5698° |
| revolutions per day: | 14.23751696 |
| mean anomaly at epoch: | 213.5569° |
| orbit number at epoch: | 23916 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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