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 39250U 13048B 23088.45270947 .00000054 00000-0 32185-3 0 9995
2 39250 82.4921 357.0963 0018260 294.0459 65.8710 12.42972089433001
| Epoch (UTC): | 29 March 2023 10:51:54 |
| Eccentricity: | 0.0018260 |
| inclination: | 82.4921° |
| perigee height: | 1479 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 357.0963° |
| argument of perigee: | 294.0459° |
| revolutions per day: | 12.42972089 |
| mean anomaly at epoch: | 65.8710° |
| orbit number at epoch: | 43300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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