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 62157U 26145.25401200 +.00000000 +00000-0 +62922-3 0 00000
2 62157 43.0024 93.1336 0001546 264.5732 95.4944 15.27607654 04
| Epoch (UTC): | 25 May 2026 06:05:46 |
| Eccentricity: | 0.0001546 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 93.1336° |
| argument of perigee: | 264.5732° |
| revolutions per day: | 15.27607654 |
| mean anomaly at epoch: | 95.4944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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