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 55821U 26145.40232388 +.00000000 +00000-0 +65677-3 0 00006
2 55821 87.8932 294.2889 0001882 87.4300 272.7046 13.14501621 05
| Epoch (UTC): | 25 May 2026 09:39:20 |
| Eccentricity: | 0.0001882 |
| inclination: | 87.8932° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2889° |
| argument of perigee: | 87.4300° |
| revolutions per day: | 13.14501621 |
| mean anomaly at epoch: | 272.7046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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