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 53570U 26145.17825670 +.00000000 +00000-0 +94945-4 0 00002
2 53570 53.2146 70.6583 0001343 69.6658 290.4478 15.08837883 08
| Epoch (UTC): | 25 May 2026 04:16:41 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 70.6583° |
| argument of perigee: | 69.6658° |
| revolutions per day: | 15.08837883 |
| mean anomaly at epoch: | 290.4478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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