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 28654U 26110.93605705 +.00000000 +00000-0 +41864-4 0 00000
2 28654 98.8115 191.4414 0013412 316.8924 43.1198 14.13718927 06
| Epoch (UTC): | 20 April 2026 22:27:55 |
| Eccentricity: | 0.0013412 |
| inclination: | 98.8115° |
| perigee height: | 837 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 191.4414° |
| argument of perigee: | 316.8924° |
| revolutions per day: | 14.13718927 |
| mean anomaly at epoch: | 43.1198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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