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 26900U 26145.28121448 +.00000000 +00000-0 +00000-0 0 00008
2 26900 6.0606 72.0568 0004501 347.8977 234.0452 1.00269837 06
| Epoch (UTC): | 25 May 2026 06:44:56 |
| Eccentricity: | 0.0004501 |
| inclination: | 6.0606° |
| perigee height: | 35768 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 72.0568° |
| argument of perigee: | 347.8977° |
| revolutions per day: | 1.00269837 |
| mean anomaly at epoch: | 234.0452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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