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 61262U 26145.54587823 +.00000000 +00000-0 +10462-3 0 00006
2 61262 53.1606 196.8398 0001142 85.2120 274.9013 15.34391341 00
| Epoch (UTC): | 25 May 2026 13:06:03 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 196.8398° |
| argument of perigee: | 85.2120° |
| revolutions per day: | 15.34391341 |
| mean anomaly at epoch: | 274.9013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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