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 57830U 26145.62513257 +.00000000 +00000-0 +56754-4 0 00006
2 57830 85.9900 270.0776 0001835 98.1315 262.0077 14.12442482 05
| Epoch (UTC): | 25 May 2026 15:00:11 |
| Eccentricity: | 0.0001835 |
| inclination: | 85.9900° |
| perigee height: | 850 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 270.0776° |
| argument of perigee: | 98.1315° |
| revolutions per day: | 14.12442482 |
| mean anomaly at epoch: | 262.0077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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