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 27646U 26069.96960448 +.00000000 +00000-0 +30329-3 0 00007
2 27646 49.5190 267.1016 5410901 125.7197 9.0824 4.61717868 01
| Epoch (UTC): | 10 March 2026 23:16:13 |
| Eccentricity: | 0.5410901 |
| inclination: | 49.5190° |
| perigee height: | 613 km |
| apogee height: | 17099 km |
| right ascension of ascending node: | 267.1016° |
| argument of perigee: | 125.7197° |
| revolutions per day: | 4.61717868 |
| mean anomaly at epoch: | 9.0824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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