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 27714U 26150.08725168 +.00000000 +00000-0 +00000-0 0 00005
2 27714 8.7883 61.2017 0010713 334.4401 236.4158 0.99812229 06
| Epoch (UTC): | 30 May 2026 02:05:38 |
| Eccentricity: | 0.0010713 |
| inclination: | 8.7883° |
| perigee height: | 35871 km |
| apogee height: | 35961 km |
| right ascension of ascending node: | 61.2017° |
| argument of perigee: | 334.4401° |
| revolutions per day: | 0.99812229 |
| mean anomaly at epoch: | 236.4158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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