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 25395U 98043B 23332.51636453 .00000484 00000-0 22313-3 0 9994
2 25395 98.8533 289.7972 0001791 296.2748 63.8247 14.25703562320046
| Epoch (UTC): | 28 November 2023 12:23:33 |
| Eccentricity: | 0.0001791 |
| inclination: | 98.8533° |
| perigee height: | 805 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 289.7972° |
| argument of perigee: | 296.2748° |
| revolutions per day: | 14.25703562 |
| mean anomaly at epoch: | 63.8247° |
| orbit number at epoch: | 32004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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