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 28059U 26040.60111352 +.00000000 +00000-0 +14651-3 0 00008
2 28059 98.6849 34.4111 0047418 318.5554 41.2049 14.54989170 07
| Epoch (UTC): | 09 February 2026 14:25:36 |
| Eccentricity: | 0.0047418 |
| inclination: | 98.6849° |
| perigee height: | 676 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 34.4111° |
| argument of perigee: | 318.5554° |
| revolutions per day: | 14.54989170 |
| mean anomaly at epoch: | 41.2049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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