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 23029.13477890 .00015460 00000-0 18308-3 0 9990
2 48274 41.4745 283.6785 0002380 70.4818 66.6540 15.60910652100083
| Epoch (UTC): | 29 January 2023 03:14:04 |
| Eccentricity: | 0.0002380 |
| inclination: | 41.4745° |
| perigee height: | 383 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 283.6785° |
| argument of perigee: | 70.4818° |
| revolutions per day: | 15.60910652 |
| mean anomaly at epoch: | 66.6540° |
| orbit number at epoch: | 10008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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