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 26880U 26145.92266970 +.00000000 +00000-0 +00000-0 0 00006
2 26880 12.7621 16.5987 0000888 96.5311 97.4019 0.99202875 02
| Epoch (UTC): | 25 May 2026 22:08:38 |
| Eccentricity: | 0.0000888 |
| inclination: | 12.7621° |
| perigee height: | 36085 km |
| apogee height: | 36093 km |
| right ascension of ascending node: | 16.5987° |
| argument of perigee: | 96.5311° |
| revolutions per day: | 0.99202875 |
| mean anomaly at epoch: | 97.4019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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