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 52137U 26145.22656547 +.00000000 +00000-0 -65887-5 0 00006
2 52137 53.2142 85.5305 0001342 95.0001 265.1144 15.08843609 05
| Epoch (UTC): | 25 May 2026 05:26:15 |
| Eccentricity: | 0.0001342 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 85.5305° |
| argument of perigee: | 95.0001° |
| revolutions per day: | 15.08843609 |
| mean anomaly at epoch: | 265.1144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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