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 62099U 26145.46960025 +.00000000 +00000-0 +14757-2 0 00005
2 62099 43.0001 299.8237 0001622 269.7520 90.3162 15.70905795 07
| Epoch (UTC): | 25 May 2026 11:16:13 |
| Eccentricity: | 0.0001622 |
| inclination: | 43.0001° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 299.8237° |
| argument of perigee: | 269.7520° |
| revolutions per day: | 15.70905795 |
| mean anomaly at epoch: | 90.3162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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