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 00020U 26135.08142491 +.00000000 +00000-0 +85845-4 0 00005
2 00020 33.3551 26.1221 1638128 236.1273 107.2707 11.61947979 09
| Epoch (UTC): | 15 May 2026 01:57:15 |
| Eccentricity: | 0.1638128 |
| inclination: | 33.3551° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 26.1221° |
| argument of perigee: | 236.1273° |
| revolutions per day: | 11.61947979 |
| mean anomaly at epoch: | 107.2707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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