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 52637U 26145.64701191 +.00000000 +00000-0 -17957-6 0 00009
2 52637 53.2155 273.6440 0001244 85.7733 274.3401 15.08832629 01
| Epoch (UTC): | 25 May 2026 15:31:41 |
| Eccentricity: | 0.0001244 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 273.6440° |
| argument of perigee: | 85.7733° |
| revolutions per day: | 15.08832629 |
| mean anomaly at epoch: | 274.3401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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