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 53836U 26145.50003470 +.00000000 +00000-0 +31904-2 0 00004
2 53836 53.2184 307.6481 0000915 117.9496 153.5310 15.27972190 02
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0000915 |
| inclination: | 53.2184° |
| perigee height: | 481 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 307.6481° |
| argument of perigee: | 117.9496° |
| revolutions per day: | 15.27972190 |
| mean anomaly at epoch: | 153.5310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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