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 60235U 24128A 25343.19971334 .00003511 00000-0 28553-3 0 9993
2 60235 61.9921 171.5633 0064410 92.3721 268.4745 14.99989856 77492
| Epoch (UTC): | 09 December 2025 04:47:35 |
| Eccentricity: | 0.0064410 |
| inclination: | 61.9921° |
| perigee height: | 522 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 171.5633° |
| argument of perigee: | 92.3721° |
| revolutions per day: | 14.99989856 |
| mean anomaly at epoch: | 268.4745° |
| orbit number at epoch: | 7749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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