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 26145.41895213 +.00000000 +00000-0 +00000-0 0 00009
2 27691 10.9185 43.6152 0004488 314.0610 274.3141 1.00275116 06
| Epoch (UTC): | 25 May 2026 10:03:17 |
| Eccentricity: | 0.0004488 |
| inclination: | 10.9185° |
| perigee height: | 35767 km |
| apogee height: | 35805 km |
| right ascension of ascending node: | 43.6152° |
| argument of perigee: | 314.0610° |
| revolutions per day: | 1.00275116 |
| mean anomaly at epoch: | 274.3141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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