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 49078U 26145.52878593 +.00000000 +00000-0 -11495-2 0 00009
2 49078 87.8958 355.1614 0001855 93.5411 266.5930 13.12441082 09
| Epoch (UTC): | 25 May 2026 12:41:27 |
| Eccentricity: | 0.0001855 |
| inclination: | 87.8958° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1614° |
| argument of perigee: | 93.5411° |
| revolutions per day: | 13.12441082 |
| mean anomaly at epoch: | 266.5930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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