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 28479U 26100.01269169 +.00000000 +00000-0 +17108-3 0 00006
2 28479 98.0608 111.2506 0010885 112.8233 247.4121 14.66407515 01
| Epoch (UTC): | 10 April 2026 00:18:16 |
| Eccentricity: | 0.0010885 |
| inclination: | 98.0608° |
| perigee height: | 665 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 111.2506° |
| argument of perigee: | 112.8233° |
| revolutions per day: | 14.66407515 |
| mean anomaly at epoch: | 247.4121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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