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 55153U 26145.49702953 +.00000000 +00000-0 +12961-3 0 00001
2 55153 87.9157 339.9872 0001988 103.8170 256.3184 13.18686932 01
| Epoch (UTC): | 25 May 2026 11:55:43 |
| Eccentricity: | 0.0001988 |
| inclination: | 87.9157° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9872° |
| argument of perigee: | 103.8170° |
| revolutions per day: | 13.18686932 |
| mean anomaly at epoch: | 256.3184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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