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 53780U 26145.66221316 +.00000000 +00000-0 +58974-4 0 00008
2 53780 53.2130 288.7715 0001104 91.1850 268.9269 15.08837840 03
| Epoch (UTC): | 25 May 2026 15:53:35 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 288.7715° |
| argument of perigee: | 91.1850° |
| revolutions per day: | 15.08837840 |
| mean anomaly at epoch: | 268.9269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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