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 27711U 26144.97222338 +.00000000 +00000-0 +00000-0 0 00004
2 27711 12.3162 30.0345 0101691 8.0259 346.6481 1.00273010 08
| Epoch (UTC): | 24 May 2026 23:20:00 |
| Eccentricity: | 0.0101691 |
| inclination: | 12.3162° |
| perigee height: | 35357 km |
| apogee height: | 36215 km |
| right ascension of ascending node: | 30.0345° |
| argument of perigee: | 8.0259° |
| revolutions per day: | 1.00273010 |
| mean anomaly at epoch: | 346.6481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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