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 26100.13984844 +.00000000 +00000-0 +63117-4 0 00001
2 27610 64.5618 3.5249 0265449 93.6793 51.0266 14.29525979 01
| Epoch (UTC): | 10 April 2026 03:21:22 |
| Eccentricity: | 0.0265449 |
| inclination: | 64.5618° |
| perigee height: | 603 km |
| apogee height: | 984 km |
| right ascension of ascending node: | 3.5249° |
| argument of perigee: | 93.6793° |
| revolutions per day: | 14.29525979 |
| mean anomaly at epoch: | 51.0266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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