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 53452U 26145.58534845 +.00000000 +00000-0 +70707-3 0 00006
2 53452 97.5488 274.9008 0001485 83.0455 277.0975 15.70058450 07
| Epoch (UTC): | 25 May 2026 14:02:54 |
| Eccentricity: | 0.0001485 |
| inclination: | 97.5488° |
| perigee height: | 358 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 274.9008° |
| argument of perigee: | 83.0455° |
| revolutions per day: | 15.70058450 |
| mean anomaly at epoch: | 277.0975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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