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 53834U 26145.51219002 +.00000000 +00000-0 -24987-4 0 00009
2 53834 53.2141 318.9211 0001281 94.5890 265.5249 15.08839221 05
| Epoch (UTC): | 25 May 2026 12:17:33 |
| Eccentricity: | 0.0001281 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 318.9211° |
| argument of perigee: | 94.5890° |
| revolutions per day: | 15.08839221 |
| mean anomaly at epoch: | 265.5249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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