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 26150.50509058 +.00000000 +00000-0 +20800-3 0 00002
2 28479 98.0574 160.8520 0008589 323.3628 36.6987 14.66485908 04
| Epoch (UTC): | 30 May 2026 12:07:19 |
| Eccentricity: | 0.0008589 |
| inclination: | 98.0574° |
| perigee height: | 666 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 160.8520° |
| argument of perigee: | 323.3628° |
| revolutions per day: | 14.66485908 |
| mean anomaly at epoch: | 36.6987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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