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 53704U 26145.02097740 +.00000000 +00000-0 +31688-4 0 00009
2 53704 53.2132 261.7100 0001142 93.1587 266.9536 15.08838491 09
| Epoch (UTC): | 25 May 2026 00:30:12 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 261.7100° |
| argument of perigee: | 93.1587° |
| revolutions per day: | 15.08838491 |
| mean anomaly at epoch: | 266.9536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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