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 27954U 26145.60781774 +.00000000 +00000-0 +00000-0 0 00008
2 27954 1.3614 84.1247 0002150 338.2604 249.6276 1.00273136 03
| Epoch (UTC): | 25 May 2026 14:35:15 |
| Eccentricity: | 0.0002150 |
| inclination: | 1.3614° |
| perigee height: | 35777 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 84.1247° |
| argument of perigee: | 338.2604° |
| revolutions per day: | 1.00273136 |
| mean anomaly at epoch: | 249.6276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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