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 25338U 98030A 22178.52278013 .00000147 00000-0 79784-4 0 9990
2 25338 98.6429 207.9265 0009142 267.8895 92.1238 14.26143389254707
| Epoch (UTC): | 27 June 2022 12:32:48 |
| Eccentricity: | 0.0009142 |
| inclination: | 98.6429° |
| perigee height: | 798 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 207.9265° |
| argument of perigee: | 267.8895° |
| revolutions per day: | 14.26143389 |
| mean anomaly at epoch: | 92.1238° |
| orbit number at epoch: | 25470 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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