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 53843U 26145.48372308 +.00000000 +00000-0 -54389-5 0 00004
2 53843 53.2148 309.4678 0000872 91.8952 268.2140 15.08833799 02
| Epoch (UTC): | 25 May 2026 11:36:33 |
| Eccentricity: | 0.0000872 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 309.4678° |
| argument of perigee: | 91.8952° |
| revolutions per day: | 15.08833799 |
| mean anomaly at epoch: | 268.2140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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