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 48274U 21035A 23028.61111762 .00016030 00000-0 18976-3 0 9990
2 48274 41.4741 286.8640 0002365 62.3075 8.4135 15.60896629100005
| Epoch (UTC): | 28 January 2023 14:40:00 |
| Eccentricity: | 0.0002365 |
| inclination: | 41.4741° |
| perigee height: | 383 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 286.8640° |
| argument of perigee: | 62.3075° |
| revolutions per day: | 15.60896629 |
| mean anomaly at epoch: | 8.4135° |
| orbit number at epoch: | 10000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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