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 26065.89295662 +.00000000 +00000-0 +88495-4 0 00003
2 28051 98.2046 107.3539 0062984 289.6748 194.4049 14.36115000 00
| Epoch (UTC): | 06 March 2026 21:25:51 |
| Eccentricity: | 0.0062984 |
| inclination: | 98.2046° |
| perigee height: | 726 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 107.3539° |
| argument of perigee: | 289.6748° |
| revolutions per day: | 14.36115000 |
| mean anomaly at epoch: | 194.4049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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