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 23343.42694148 .00012059 00000-0 13034-3 0 9990
2 48274 41.4689 168.6261 0007738 302.7708 57.2386 15.63415377149233
| Epoch (UTC): | 09 December 2023 10:14:47 |
| Eccentricity: | 0.0007738 |
| inclination: | 41.4689° |
| perigee height: | 372 km |
| apogee height: | 383 km |
| right ascension of ascending node: | 168.6261° |
| argument of perigee: | 302.7708° |
| revolutions per day: | 15.63415377 |
| mean anomaly at epoch: | 57.2386° |
| orbit number at epoch: | 14923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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