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 59137U 26145.61003045 +.00000000 +00000-0 +14037-3 0 00003
2 59137 97.5584 282.2804 0009772 322.7915 37.2645 15.27399130 02
| Epoch (UTC): | 25 May 2026 14:38:26 |
| Eccentricity: | 0.0009772 |
| inclination: | 97.5584° |
| perigee height: | 477 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 282.2804° |
| argument of perigee: | 322.7915° |
| revolutions per day: | 15.27399130 |
| mean anomaly at epoch: | 37.2645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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