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 53760U 26145.38068837 +.00000000 +00000-0 +35362-3 0 00007
2 53760 35.0057 122.3599 0004111 117.3723 242.7411 15.23137147 00
| Epoch (UTC): | 25 May 2026 09:08:11 |
| Eccentricity: | 0.0004111 |
| inclination: | 35.0057° |
| perigee height: | 494 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 122.3599° |
| argument of perigee: | 117.3723° |
| revolutions per day: | 15.23137147 |
| mean anomaly at epoch: | 242.7411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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