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 6180U 72069B 25312.68227098 .00004043 00000-0 60160-3 0 9991
2 6180 90.0602 218.7394 0032848 206.8028 153.1497 14.74458628795199
| Epoch (UTC): | 08 November 2025 16:22:28 |
| Eccentricity: | 0.0032848 |
| inclination: | 90.0602° |
| perigee height: | 624 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 218.7394° |
| argument of perigee: | 206.8028° |
| revolutions per day: | 14.74458628 |
| mean anomaly at epoch: | 153.1497° |
| orbit number at epoch: | 79519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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