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 49753U 26145.36272939 +.00000000 +00000-0 +42750-4 0 00002
2 49753 53.2122 164.9234 0001081 70.8858 289.2251 15.08837179 08
| Epoch (UTC): | 25 May 2026 08:42:19 |
| Eccentricity: | 0.0001081 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.9234° |
| argument of perigee: | 70.8858° |
| revolutions per day: | 15.08837179 |
| mean anomaly at epoch: | 289.2251° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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