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 53234U 26145.66668980 +.00000000 +00000-0 +99027-2 0 00006
2 53234 97.6032 206.4630 0001614 81.2993 80.1041 15.26319482 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001614 |
| inclination: | 97.6032° |
| perigee height: | 486 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 206.4630° |
| argument of perigee: | 81.2993° |
| revolutions per day: | 15.26319482 |
| mean anomaly at epoch: | 80.1041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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