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 49765U 26145.41244598 +.00000000 +00000-0 +66650-4 0 00006
2 49765 53.2128 154.7106 0001186 71.8387 288.2735 15.08838097 02
| Epoch (UTC): | 25 May 2026 09:53:55 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.7106° |
| argument of perigee: | 71.8387° |
| revolutions per day: | 15.08838097 |
| mean anomaly at epoch: | 288.2735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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