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 49768U 26145.43356596 +.00000000 +00000-0 +19132-4 0 00006
2 49768 53.2136 154.6045 0001476 60.4830 299.6309 15.08840259 00
| Epoch (UTC): | 25 May 2026 10:24:20 |
| Eccentricity: | 0.0001476 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.6045° |
| argument of perigee: | 60.4830° |
| revolutions per day: | 15.08840259 |
| mean anomaly at epoch: | 299.6309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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