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 26262U 26099.78093622 +.00000000 +00000-0 +91008-3 0 00005
2 26262 98.3313 196.9994 0037776 5.2402 119.3265 14.81849264 01
| Epoch (UTC): | 09 April 2026 18:44:32 |
| Eccentricity: | 0.0037776 |
| inclination: | 98.3313° |
| perigee height: | 597 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 196.9994° |
| argument of perigee: | 5.2402° |
| revolutions per day: | 14.81849264 |
| mean anomaly at epoch: | 119.3265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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