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 39416U 13066A 25073.61925953 .00004852 00000-0 50760-3 0 9996
2 39416 97.7113 30.8792 0035542 295.5139 64.2404 14.89632019612760
| Epoch (UTC): | 14 March 2025 14:51:44 |
| Eccentricity: | 0.0035542 |
| inclination: | 97.7113° |
| perigee height: | 574 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 30.8792° |
| argument of perigee: | 295.5139° |
| revolutions per day: | 14.89632019 |
| mean anomaly at epoch: | 64.2404° |
| orbit number at epoch: | 61276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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