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 00900U 26145.58369744 +.00000000 +00000-0 +57619-3 0 00007
2 00900 90.2237 71.2377 0026984 6.5488 168.2941 13.76595064 08
| Epoch (UTC): | 25 May 2026 14:00:31 |
| Eccentricity: | 0.0026984 |
| inclination: | 90.2237° |
| perigee height: | 956 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 71.2377° |
| argument of perigee: | 6.5488° |
| revolutions per day: | 13.76595064 |
| mean anomaly at epoch: | 168.2941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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