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 23271.95138419 .00021942 00000-0 23606-3 0 9999
2 48274 41.4725 244.4535 0008543 140.5762 219.5701 15.63162984138059
| Epoch (UTC): | 28 September 2023 22:49:59 |
| Eccentricity: | 0.0008543 |
| inclination: | 41.4725° |
| perigee height: | 373 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 244.4535° |
| argument of perigee: | 140.5762° |
| revolutions per day: | 15.63162984 |
| mean anomaly at epoch: | 219.5701° |
| orbit number at epoch: | 13805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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