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 53071U 26145.41916146 +.00000000 +00000-0 +26916-3 0 00006
2 53071 97.4455 326.5397 0001351 92.4909 267.6473 15.05636643 04
| Epoch (UTC): | 25 May 2026 10:03:35 |
| Eccentricity: | 0.0001351 |
| inclination: | 97.4455° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 326.5397° |
| argument of perigee: | 92.4909° |
| revolutions per day: | 15.05636643 |
| mean anomaly at epoch: | 267.6473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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