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 25198.18364684 .00009831 00000-0 13757-3 0 9998
2 48274 41.4640 198.7361 0008404 293.7813 66.2143 15.56780247240834
| Epoch (UTC): | 17 July 2025 04:24:27 |
| Eccentricity: | 0.0008404 |
| inclination: | 41.4640° |
| perigee height: | 391 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 198.7361° |
| argument of perigee: | 293.7813° |
| revolutions per day: | 15.56780247 |
| mean anomaly at epoch: | 66.2143° |
| orbit number at epoch: | 24083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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