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 26032.44625449 +.00000000 +00000-0 +61211-4 0 00004
2 28654 98.8220 114.0498 0014485 172.8400 187.2982 14.13702650 03
| Epoch (UTC): | 01 February 2026 10:42:36 |
| Eccentricity: | 0.0014485 |
| inclination: | 98.8220° |
| perigee height: | 836 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 114.0498° |
| argument of perigee: | 172.8400° |
| revolutions per day: | 14.13702650 |
| mean anomaly at epoch: | 187.2982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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