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 28899U 26144.97049005 +.00000000 +00000-0 +00000-0 0 00000
2 28899 5.0664 43.7388 0003099 17.9205 313.7656 1.00271591 04
| Epoch (UTC): | 24 May 2026 23:17:30 |
| Eccentricity: | 0.0003099 |
| inclination: | 5.0664° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 43.7388° |
| argument of perigee: | 17.9205° |
| revolutions per day: | 1.00271591 |
| mean anomaly at epoch: | 313.7656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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