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 53506U 26145.66668980 +.00000000 +00000-0 +11903-1 0 00004
2 53506 97.6031 268.9658 0001338 89.1198 16.5850 15.45396262 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001338 |
| inclination: | 97.6031° |
| perigee height: | 429 km |
| apogee height: | 431 km |
| right ascension of ascending node: | 268.9658° |
| argument of perigee: | 89.1198° |
| revolutions per day: | 15.45396262 |
| mean anomaly at epoch: | 16.5850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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