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 65989U 26145.53398550 +.00000000 +00000-0 +11130-3 0 00005
2 65989 81.3037 232.6209 0001977 254.1236 105.9703 13.84855874 00
| Epoch (UTC): | 25 May 2026 12:48:56 |
| Eccentricity: | 0.0001977 |
| inclination: | 81.3037° |
| perigee height: | 945 km |
| apogee height: | 948 km |
| right ascension of ascending node: | 232.6209° |
| argument of perigee: | 254.1236° |
| revolutions per day: | 13.84855874 |
| mean anomaly at epoch: | 105.9703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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