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 65324U 26145.37140818 +.00000000 +00000-0 +26636-1 0 00007
2 65324 53.1599 210.1009 0007349 228.5672 131.4699 15.33296562 07
| Epoch (UTC): | 25 May 2026 08:54:49 |
| Eccentricity: | 0.0007349 |
| inclination: | 53.1599° |
| perigee height: | 461 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 210.1009° |
| argument of perigee: | 228.5672° |
| revolutions per day: | 15.33296562 |
| mean anomaly at epoch: | 131.4699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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