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 27465U 26145.55653969 +.00000000 +00000-0 -46563-4 0 00002
2 27465 82.4854 355.6514 0025679 303.7996 56.0640 12.44945597 03
| Epoch (UTC): | 25 May 2026 13:21:25 |
| Eccentricity: | 0.0025679 |
| inclination: | 82.4854° |
| perigee height: | 1466 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 355.6514° |
| argument of perigee: | 303.7996° |
| revolutions per day: | 12.44945597 |
| mean anomaly at epoch: | 56.0640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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