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 25117.95029429 .00044406 00000-0 49590-3 0 9990
2 48274 41.4647 326.2133 0003026 245.3246 114.7279 15.61964324228307
| Epoch (UTC): | 27 April 2025 22:48:25 |
| Eccentricity: | 0.0003026 |
| inclination: | 41.4647° |
| perigee height: | 380 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 326.2133° |
| argument of perigee: | 245.3246° |
| revolutions per day: | 15.61964324 |
| mean anomaly at epoch: | 114.7279° |
| orbit number at epoch: | 22830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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