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 is defined by the following mean orbital elements,
1 60534U 26145.49033811 +.00000000 +00000-0 +20125-3 0 00001
2 60534 97.6832 220.8611 0001933 109.8688 250.2742 14.96262394 09
| Epoch (UTC): | 25 May 2026 11:46:05 |
| Eccentricity: | 0.0001933 |
| inclination: | 97.6832° |
| perigee height: | 577 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 220.8611° |
| argument of perigee: | 109.8688° |
| revolutions per day: | 14.96262394 |
| mean anomaly at epoch: | 250.2742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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