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 65581U 26145.65072677 +.00000000 +00000-0 +15553-3 0 00008
2 65581 81.3039 31.3799 0008756 253.6679 106.3515 13.84772212 05
| Epoch (UTC): | 25 May 2026 15:37:02 |
| Eccentricity: | 0.0008756 |
| inclination: | 81.3039° |
| perigee height: | 941 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 31.3799° |
| argument of perigee: | 253.6679° |
| revolutions per day: | 13.84772212 |
| mean anomaly at epoch: | 106.3515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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