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 53034U 26145.53803241 +.00000000 +00000-0 +36734-4 0 00009
2 53034 53.2122 89.1806 0001316 78.9192 281.1948 15.08835823 07
| Epoch (UTC): | 25 May 2026 12:54:46 |
| Eccentricity: | 0.0001316 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 89.1806° |
| argument of perigee: | 78.9192° |
| revolutions per day: | 15.08835823 |
| mean anomaly at epoch: | 281.1948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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