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 40019U 26145.33743345 +.00000000 +00000-0 +59878-4 0 00008
2 40019 97.9619 272.8107 0078460 347.7574 12.1724 14.70859992 07
| Epoch (UTC): | 25 May 2026 08:05:54 |
| Eccentricity: | 0.0078460 |
| inclination: | 97.9619° |
| perigee height: | 603 km |
| apogee height: | 714 km |
| right ascension of ascending node: | 272.8107° |
| argument of perigee: | 347.7574° |
| revolutions per day: | 14.70859992 |
| mean anomaly at epoch: | 12.1724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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