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 55835U 26145.45430082 +.00000000 +00000-0 +71572-4 0 00009
2 55835 87.9151 309.5098 0001544 87.5126 272.6183 13.19726445 07
| Epoch (UTC): | 25 May 2026 10:54:11 |
| Eccentricity: | 0.0001544 |
| inclination: | 87.9151° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5098° |
| argument of perigee: | 87.5126° |
| revolutions per day: | 13.19726445 |
| mean anomaly at epoch: | 272.6183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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