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 38254U 26146.08169703 +.00000000 +00000-0 +00000-0 0 00008
2 38254 6.6004 57.6484 0002413 357.5906 201.3663 1.00271358 07
| Epoch (UTC): | 26 May 2026 01:57:38 |
| Eccentricity: | 0.0002413 |
| inclination: | 6.6004° |
| perigee height: | 35777 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 57.6484° |
| argument of perigee: | 357.5906° |
| revolutions per day: | 1.00271358 |
| mean anomaly at epoch: | 201.3663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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