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 60548U 26044.71222456 +.00000000 +00000-0 +36112-3 0 00007
2 60548 97.7061 124.7519 0005574 185.4781 174.6383 15.00879468 09
| Epoch (UTC): | 13 February 2026 17:05:36 |
| Eccentricity: | 0.0005574 |
| inclination: | 97.7061° |
| perigee height: | 560 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 124.7519° |
| argument of perigee: | 185.4781° |
| revolutions per day: | 15.00879468 |
| mean anomaly at epoch: | 174.6383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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