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 26857U 26150.13768748 +.00000000 +00000-0 +00000-0 0 00009
2 26857 44.8356 249.4246 0014887 50.2754 309.8960 3.92401628 02
| Epoch (UTC): | 30 May 2026 03:18:16 |
| Eccentricity: | 0.0014887 |
| inclination: | 44.8356° |
| perigee height: | 10576 km |
| apogee height: | 10626 km |
| right ascension of ascending node: | 249.4246° |
| argument of perigee: | 50.2754° |
| revolutions per day: | 3.92401628 |
| mean anomaly at epoch: | 309.8960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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