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 27640U 26041.49940512 +.00000000 +00000-0 +96563-4 0 00002
2 27640 98.7157 50.3061 0013352 214.3531 145.6783 14.19901442 05
| Epoch (UTC): | 10 February 2026 11:59:08 |
| Eccentricity: | 0.0013352 |
| inclination: | 98.7157° |
| perigee height: | 816 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 50.3061° |
| argument of perigee: | 214.3531° |
| revolutions per day: | 14.19901442 |
| mean anomaly at epoch: | 145.6783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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