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 44881U 19093C 25140.55544269 .00000873 00000-0 10706-3 0 9994
2 44881 97.7926 216.6235 0012462 300.3619 59.6364 14.85560514293106
| Epoch (UTC): | 20 May 2025 13:19:50 |
| Eccentricity: | 0.0012462 |
| inclination: | 97.7926° |
| perigee height: | 603 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 216.6235° |
| argument of perigee: | 300.3619° |
| revolutions per day: | 14.85560514 |
| mean anomaly at epoch: | 59.6364° |
| orbit number at epoch: | 29310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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