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 39497U 13076E 23088.51751375 .00000024 00000-0 10000-3 0 9994
2 39497 82.4916 181.5680 0014059 133.4793 226.7455 12.43465262419899
| Epoch (UTC): | 29 March 2023 12:25:13 |
| Eccentricity: | 0.0014059 |
| inclination: | 82.4916° |
| perigee height: | 1481 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 181.5680° |
| argument of perigee: | 133.4793° |
| revolutions per day: | 12.43465262 |
| mean anomaly at epoch: | 226.7455° |
| orbit number at epoch: | 41989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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