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 55159U 26145.57219154 +.00000000 +00000-0 +21575-3 0 00003
2 55159 86.9116 186.8130 0013353 30.5055 329.6959 15.12944710 05
| Epoch (UTC): | 25 May 2026 13:43:57 |
| Eccentricity: | 0.0013353 |
| inclination: | 86.9116° |
| perigee height: | 518 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 186.8130° |
| argument of perigee: | 30.5055° |
| revolutions per day: | 15.12944710 |
| mean anomaly at epoch: | 329.6959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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