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 00902U 26145.57336647 +.00000000 +00000-0 +78469-4 0 00001
2 00902 90.2373 75.2506 0016771 296.2915 250.7719 13.52898349 01
| Epoch (UTC): | 25 May 2026 13:45:38 |
| Eccentricity: | 0.0016771 |
| inclination: | 90.2373° |
| perigee height: | 1049 km |
| apogee height: | 1074 km |
| right ascension of ascending node: | 75.2506° |
| argument of perigee: | 296.2915° |
| revolutions per day: | 13.52898349 |
| mean anomaly at epoch: | 250.7719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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