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 53837U 26145.18468678 +.00000000 +00000-0 +86284-3 0 00006
2 53837 53.2137 320.4317 0001363 107.4094 252.7047 15.08771576 01
| Epoch (UTC): | 25 May 2026 04:25:56 |
| Eccentricity: | 0.0001363 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 320.4317° |
| argument of perigee: | 107.4094° |
| revolutions per day: | 15.08771576 |
| mean anomaly at epoch: | 252.7047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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