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 53037U 26145.11757689 +.00000000 +00000-0 -14632-3 0 00003
2 53037 53.2155 91.0212 0001810 95.7048 264.4150 15.08827765 00
| Epoch (UTC): | 25 May 2026 02:49:18 |
| Eccentricity: | 0.0001810 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 91.0212° |
| argument of perigee: | 95.7048° |
| revolutions per day: | 15.08827765 |
| mean anomaly at epoch: | 264.4150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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