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 57943U 26145.39544637 +.00000000 +00000-0 +16168-3 0 00005
2 57943 53.1618 28.1808 0001546 105.5783 254.5389 15.30166774 02
| Epoch (UTC): | 25 May 2026 09:29:26 |
| Eccentricity: | 0.0001546 |
| inclination: | 53.1618° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 28.1808° |
| argument of perigee: | 105.5783° |
| revolutions per day: | 15.30166774 |
| mean anomaly at epoch: | 254.5389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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