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 28051U 26114.30891183 +.00000000 +00000-0 +33312-4 0 00002
2 28051 98.1959 153.4494 0064906 142.9885 309.5939 14.36141234 08
| Epoch (UTC): | 24 April 2026 07:24:49 |
| Eccentricity: | 0.0064906 |
| inclination: | 98.1959° |
| perigee height: | 725 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 153.4494° |
| argument of perigee: | 142.9885° |
| revolutions per day: | 14.36141234 |
| mean anomaly at epoch: | 309.5939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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