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 53158U 26145.49935031 +.00000000 +00000-0 -50885-5 0 00009
2 53158 53.2127 179.3067 0001138 76.3478 283.7641 15.08837588 09
| Epoch (UTC): | 25 May 2026 11:59:03 |
| Eccentricity: | 0.0001138 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.3067° |
| argument of perigee: | 76.3478° |
| revolutions per day: | 15.08837588 |
| mean anomaly at epoch: | 283.7641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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