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 53137U 26145.50947160 +.00000000 +00000-0 -16404-4 0 00002
2 53137 53.2136 189.2586 0001196 97.6035 262.5094 15.08834542 05
| Epoch (UTC): | 25 May 2026 12:13:38 |
| Eccentricity: | 0.0001196 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.2586° |
| argument of perigee: | 97.6035° |
| revolutions per day: | 15.08834542 |
| mean anomaly at epoch: | 262.5094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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