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 27610U 26069.13343274 +.00000000 +00000-0 +41958-4 0 00000
2 27610 64.5579 91.6593 0265864 102.4801 323.1432 14.29511215 03
| Epoch (UTC): | 10 March 2026 03:12:08 |
| Eccentricity: | 0.0265864 |
| inclination: | 64.5579° |
| perigee height: | 603 km |
| apogee height: | 984 km |
| right ascension of ascending node: | 91.6593° |
| argument of perigee: | 102.4801° |
| revolutions per day: | 14.29511215 |
| mean anomaly at epoch: | 323.1432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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