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 49758U 26145.33421141 +.00000000 +00000-0 +15335-4 0 00004
2 49758 53.2128 155.0491 0001318 81.7092 278.4049 15.08837187 03
| Epoch (UTC): | 25 May 2026 08:01:15 |
| Eccentricity: | 0.0001318 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 155.0491° |
| argument of perigee: | 81.7092° |
| revolutions per day: | 15.08837187 |
| mean anomaly at epoch: | 278.4049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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