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 49440U 26145.59272132 +.00000000 +00000-0 +15050-3 0 00007
2 49440 53.2130 223.8894 0001380 76.5813 283.5333 15.08847676 04
| Epoch (UTC): | 25 May 2026 14:13:31 |
| Eccentricity: | 0.0001380 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 223.8894° |
| argument of perigee: | 76.5813° |
| revolutions per day: | 15.08847676 |
| mean anomaly at epoch: | 283.5333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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