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 53049U 26145.38181156 +.00000000 +00000-0 +65331-3 0 00006
2 53049 97.4474 325.2869 0001273 94.1461 265.9911 15.05610341 00
| Epoch (UTC): | 25 May 2026 09:09:48 |
| Eccentricity: | 0.0001273 |
| inclination: | 97.4474° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 325.2869° |
| argument of perigee: | 94.1461° |
| revolutions per day: | 15.05610341 |
| mean anomaly at epoch: | 265.9911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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