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 28621U 26088.05888926 +.00000000 +00000-0 +38308-2 0 00006
2 28621 100.2452 308.8123 0028689 78.9628 281.4773 14.30304509 04
| Epoch (UTC): | 29 March 2026 01:24:48 |
| Eccentricity: | 0.0028689 |
| inclination: | 100.2452° |
| perigee height: | 770 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 308.8123° |
| argument of perigee: | 78.9628° |
| revolutions per day: | 14.30304509 |
| mean anomaly at epoch: | 281.4773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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