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 26121.43862888 +.00000000 +00000-0 +00000-0 0 00004
2 25933 51.5069 297.5125 0106527 173.4996 193.3108 2.00564783 01
| Epoch (UTC): | 01 May 2026 10:31:37 |
| Eccentricity: | 0.0106527 |
| inclination: | 51.5069° |
| perigee height: | 19899 km |
| apogee height: | 20465 km |
| right ascension of ascending node: | 297.5125° |
| argument of perigee: | 173.4996° |
| revolutions per day: | 2.00564783 |
| mean anomaly at epoch: | 193.3108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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