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 53838U 26145.15989095 +.00000000 +00000-0 +33834-4 0 00009
2 53838 53.2121 310.9992 0001535 98.5659 261.5507 15.08835918 06
| Epoch (UTC): | 25 May 2026 03:50:14 |
| Eccentricity: | 0.0001535 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 310.9992° |
| argument of perigee: | 98.5659° |
| revolutions per day: | 15.08835918 |
| mean anomaly at epoch: | 261.5507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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