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 55157U 26145.36218756 +.00000000 +00000-0 -97299-4 0 00003
2 55157 87.9154 10.4068 0001840 54.6345 305.4958 13.17648785 02
| Epoch (UTC): | 25 May 2026 08:41:33 |
| Eccentricity: | 0.0001840 |
| inclination: | 87.9154° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4068° |
| argument of perigee: | 54.6345° |
| revolutions per day: | 13.17648785 |
| mean anomaly at epoch: | 305.4958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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