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 69028U 26145.59409205 +.00000000 +00000-0 +64902-3 0 00004
2 69028 97.2848 0.3624 0001177 86.6768 273.4632 15.75219258 09
| Epoch (UTC): | 25 May 2026 14:15:29 |
| Eccentricity: | 0.0001177 |
| inclination: | 97.2848° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 0.3624° |
| argument of perigee: | 86.6768° |
| revolutions per day: | 15.75219258 |
| mean anomaly at epoch: | 273.4632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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