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 60577U 26145.49660214 +.00000000 +00000-0 +67703-3 0 00004
2 60577 97.6746 226.6223 0003367 202.3667 157.7415 15.08720305 05
| Epoch (UTC): | 25 May 2026 11:55:06 |
| Eccentricity: | 0.0003367 |
| inclination: | 97.6746° |
| perigee height: | 538 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 226.6223° |
| argument of perigee: | 202.3667° |
| revolutions per day: | 15.08720305 |
| mean anomaly at epoch: | 157.7415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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