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 28935U 26145.56197500 +.00000000 +00000-0 +00000-0 0 00001
2 28935 0.0257 20.0662 0001937 6.1526 309.0436 1.00271668 05
| Epoch (UTC): | 25 May 2026 13:29:14 |
| Eccentricity: | 0.0001937 |
| inclination: | 0.0257° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 20.0662° |
| argument of perigee: | 6.1526° |
| revolutions per day: | 1.00271668 |
| mean anomaly at epoch: | 309.0436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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