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 55499U 26145.35264162 +.00000000 +00000-0 +95658-4 0 00009
2 55499 42.9988 266.4471 0001334 281.0311 79.0390 15.27585716 06
| Epoch (UTC): | 25 May 2026 08:27:48 |
| Eccentricity: | 0.0001334 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.4471° |
| argument of perigee: | 281.0311° |
| revolutions per day: | 15.27585716 |
| mean anomaly at epoch: | 79.0390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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