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 02861U 26088.07841826 +.00000000 +00000-0 +44950-2 0 00004
2 02861 89.9834 314.1582 0072278 178.5693 181.5360 8.36661145 03
| Epoch (UTC): | 29 March 2026 01:52:55 |
| Eccentricity: | 0.0072278 |
| inclination: | 89.9834° |
| perigee height: | 3797 km |
| apogee height: | 3945 km |
| right ascension of ascending node: | 314.1582° |
| argument of perigee: | 178.5693° |
| revolutions per day: | 8.36661145 |
| mean anomaly at epoch: | 181.5360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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