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 01360U 65034B 25341.49360712 .00000003 00000-0 00000-0 0 9998
2 01360 32.1058 134.1724 3963601 242.2174 72.3209 4.64830595 28954
| Epoch (UTC): | 07 December 2025 11:50:47 |
| Eccentricity: | 0.3963601 |
| inclination: | 32.1058° |
| perigee height: | 2776 km |
| apogee height: | 14799 km |
| right ascension of ascending node: | 134.1724° |
| argument of perigee: | 242.2174° |
| revolutions per day: | 4.64830595 |
| mean anomaly at epoch: | 72.3209° |
| orbit number at epoch: | 2895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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