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 25984U 99065E 23083.17862507 .00007335 00000-0 26434-2 0 9998
2 25984 45.0416 343.5873 0002188 173.6406 186.4469 14.34145343217144
| Epoch (UTC): | 24 March 2023 04:17:13 |
| Eccentricity: | 0.0002188 |
| inclination: | 45.0416° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 343.5873° |
| argument of perigee: | 173.6406° |
| revolutions per day: | 14.34145343 |
| mean anomaly at epoch: | 186.4469° |
| orbit number at epoch: | 21714 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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