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 27691U 26140.34824986 +.00000000 +00000-0 +00000-0 0 00005
2 27691 10.9086 43.6581 0004411 309.6885 248.1480 1.00275041 04
| Epoch (UTC): | 20 May 2026 08:21:28 |
| Eccentricity: | 0.0004411 |
| inclination: | 10.9086° |
| perigee height: | 35767 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 43.6581° |
| argument of perigee: | 309.6885° |
| revolutions per day: | 1.00275041 |
| mean anomaly at epoch: | 248.1480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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