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 55494U 26145.38476153 +.00000000 +00000-0 +78913-4 0 00007
2 55494 43.0046 266.6927 0001464 288.6086 71.4606 15.27590831 02
| Epoch (UTC): | 25 May 2026 09:14:03 |
| Eccentricity: | 0.0001464 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.6927° |
| argument of perigee: | 288.6086° |
| revolutions per day: | 15.27590831 |
| mean anomaly at epoch: | 71.4606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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