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 65843U 26145.13327551 +.00000000 +00000-0 +74087-3 0 00003
2 65843 53.1582 92.8146 0001142 95.7457 264.3676 15.34405232 00
| Epoch (UTC): | 25 May 2026 03:11:55 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.1582° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.8146° |
| argument of perigee: | 95.7457° |
| revolutions per day: | 15.34405232 |
| mean anomaly at epoch: | 264.3676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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