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 26031.76529133 +.00000000 +00000-0 -87014-2 0 00001
2 02861 89.9956 314.1814 0071951 232.1414 127.2897 8.36660805 05
| Epoch (UTC): | 31 January 2026 18:22:01 |
| Eccentricity: | 0.0071951 |
| inclination: | 89.9956° |
| perigee height: | 3798 km |
| apogee height: | 3945 km |
| right ascension of ascending node: | 314.1814° |
| argument of perigee: | 232.1414° |
| revolutions per day: | 8.36660805 |
| mean anomaly at epoch: | 127.2897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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