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 60527U 26145.14913545 +.00000000 +00000-0 +35089-3 0 00001
2 60527 97.3724 226.6396 0006924 29.0367 331.1260 15.35508737 06
| Epoch (UTC): | 25 May 2026 03:34:45 |
| Eccentricity: | 0.0006924 |
| inclination: | 97.3724° |
| perigee height: | 455 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 226.6396° |
| argument of perigee: | 29.0367° |
| revolutions per day: | 15.35508737 |
| mean anomaly at epoch: | 331.1260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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