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 57036U 26145.59873852 +.00000000 +00000-0 +18429-3 0 00006
2 57036 97.4853 251.3604 0007991 149.4879 210.6822 15.19124759 03
| Epoch (UTC): | 25 May 2026 14:22:11 |
| Eccentricity: | 0.0007991 |
| inclination: | 97.4853° |
| perigee height: | 503 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 251.3604° |
| argument of perigee: | 149.4879° |
| revolutions per day: | 15.19124759 |
| mean anomaly at epoch: | 210.6822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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