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 52459U 26145.51453005 +.00000000 +00000-0 +11426-3 0 00006
2 52459 53.2123 74.2398 0001263 90.6492 269.4645 15.08837341 04
| Epoch (UTC): | 25 May 2026 12:20:55 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.2398° |
| argument of perigee: | 90.6492° |
| revolutions per day: | 15.08837341 |
| mean anomaly at epoch: | 269.4645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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