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 26072.57599883 +.00000000 +00000-0 +48876-4 0 00006
2 28654 98.8151 153.6287 0015198 65.2528 295.0224 14.13711684 03
| Epoch (UTC): | 13 March 2026 13:49:26 |
| Eccentricity: | 0.0015198 |
| inclination: | 98.8151° |
| perigee height: | 836 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 153.6287° |
| argument of perigee: | 65.2528° |
| revolutions per day: | 14.13711684 |
| mean anomaly at epoch: | 295.0224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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