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 25933U 26145.36984868 +.00000000 +00000-0 +00000-0 0 00005
2 25933 51.4851 296.4662 0106644 174.5329 192.0994 2.00563425 06
| Epoch (UTC): | 25 May 2026 08:52:34 |
| Eccentricity: | 0.0106644 |
| inclination: | 51.4851° |
| perigee height: | 19899 km |
| apogee height: | 20465 km |
| right ascension of ascending node: | 296.4662° |
| argument of perigee: | 174.5329° |
| revolutions per day: | 2.00563425 |
| mean anomaly at epoch: | 192.0994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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