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 62999U 26144.84379662 +.00000000 +00000-0 +59331-3 0 00004
2 62999 43.0031 73.1163 0000584 289.9441 70.1348 15.27595423 09
| Epoch (UTC): | 24 May 2026 20:15:04 |
| Eccentricity: | 0.0000584 |
| inclination: | 43.0031° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 73.1163° |
| argument of perigee: | 289.9441° |
| revolutions per day: | 15.27595423 |
| mean anomaly at epoch: | 70.1348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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