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 62615U 26145.19113208 +.00000000 +00000-0 +25581-3 0 00000
2 62615 97.3943 225.4146 0007401 59.8420 300.3550 15.25452363 03
| Epoch (UTC): | 25 May 2026 04:35:13 |
| Eccentricity: | 0.0007401 |
| inclination: | 97.3943° |
| perigee height: | 484 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 225.4146° |
| argument of perigee: | 59.8420° |
| revolutions per day: | 15.25452363 |
| mean anomaly at epoch: | 300.3550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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