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 26145.43692971 +.00000000 +00000-0 +66094-4 0 00000
2 27640 98.7129 152.6691 0012793 279.4325 80.5405 14.19937846 05
| Epoch (UTC): | 25 May 2026 10:29:10 |
| Eccentricity: | 0.0012793 |
| inclination: | 98.7129° |
| perigee height: | 816 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 152.6691° |
| argument of perigee: | 279.4325° |
| revolutions per day: | 14.19937846 |
| mean anomaly at epoch: | 80.5405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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