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 23083.47360013 .00000314 00000-0 15683-3 0 9994
2 25397 98.8594 40.2451 0002004 50.4128 309.7226 14.23844679283272
| Epoch (UTC): | 24 March 2023 11:21:59 |
| Eccentricity: | 0.0002004 |
| inclination: | 98.8594° |
| perigee height: | 811 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 40.2451° |
| argument of perigee: | 50.4128° |
| revolutions per day: | 14.23844679 |
| mean anomaly at epoch: | 309.7226° |
| orbit number at epoch: | 28327 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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