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 54692U 26145.60843416 +.00000000 +00000-0 +31117-3 0 00005
2 54692 97.6916 314.2677 0007545 189.0502 171.0604 15.33286545 03
| Epoch (UTC): | 25 May 2026 14:36:08 |
| Eccentricity: | 0.0007545 |
| inclination: | 97.6916° |
| perigee height: | 461 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 314.2677° |
| argument of perigee: | 189.0502° |
| revolutions per day: | 15.33286545 |
| mean anomaly at epoch: | 171.0604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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