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 22828U 26155.09696590 +.00000000 +00000-0 +81666-4 0 00009
2 22828 98.6858 222.4395 0010972 86.2152 274.0285 14.31792578 03
| Epoch (UTC): | 04 June 2026 02:19:37 |
| Eccentricity: | 0.0010972 |
| inclination: | 98.6858° |
| perigee height: | 778 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 222.4395° |
| argument of perigee: | 86.2152° |
| revolutions per day: | 14.31792578 |
| mean anomaly at epoch: | 274.0285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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