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 62084U 26145.51488869 +.00000000 +00000-0 +13124-3 0 00004
2 62084 97.9021 305.4363 0005577 32.3610 327.7939 14.72026565 01
| Epoch (UTC): | 25 May 2026 12:21:26 |
| Eccentricity: | 0.0005577 |
| inclination: | 97.9021° |
| perigee height: | 651 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 305.4363° |
| argument of perigee: | 32.3610° |
| revolutions per day: | 14.72026565 |
| mean anomaly at epoch: | 327.7939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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