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 44857U 26145.54532367 +.00000000 +00000-0 +21592-3 0 00006
2 44857 36.9598 245.9654 0012229 343.8474 16.1877 15.01531640 00
| Epoch (UTC): | 25 May 2026 13:05:15 |
| Eccentricity: | 0.0012229 |
| inclination: | 36.9598° |
| perigee height: | 554 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 245.9654° |
| argument of perigee: | 343.8474° |
| revolutions per day: | 15.01531640 |
| mean anomaly at epoch: | 16.1877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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