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 53085U 26145.45791990 +.00000000 +00000-0 -14221-3 0 00000
2 53085 97.4477 326.4469 0000766 78.9959 281.1354 15.05657071 02
| Epoch (UTC): | 25 May 2026 10:59:24 |
| Eccentricity: | 0.0000766 |
| inclination: | 97.4477° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 326.4469° |
| argument of perigee: | 78.9959° |
| revolutions per day: | 15.05657071 |
| mean anomaly at epoch: | 281.1354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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