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 55151U 26145.58660544 +.00000000 +00000-0 +19996-4 0 00004
2 55151 87.9151 10.3605 0001658 89.5297 270.6025 13.17650559 09
| Epoch (UTC): | 25 May 2026 14:04:42 |
| Eccentricity: | 0.0001658 |
| inclination: | 87.9151° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3605° |
| argument of perigee: | 89.5297° |
| revolutions per day: | 13.17650559 |
| mean anomaly at epoch: | 270.6025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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