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 01002U 26101.52637950 +.00000000 +00000-0 -12359-2 0 00006
2 01002 32.1407 202.6302 0015465 29.4374 330.6992 9.88355105 03
| Epoch (UTC): | 11 April 2026 12:37:59 |
| Eccentricity: | 0.0015465 |
| inclination: | 32.1407° |
| perigee height: | 2780 km |
| apogee height: | 2808 km |
| right ascension of ascending node: | 202.6302° |
| argument of perigee: | 29.4374° |
| revolutions per day: | 9.88355105 |
| mean anomaly at epoch: | 330.6992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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