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 64819U 26145.15518867 +.00000000 +00000-0 +30751-3 0 00009
2 64819 51.8965 304.9193 0000707 126.5752 233.5276 14.79935746 08
| Epoch (UTC): | 25 May 2026 03:43:28 |
| Eccentricity: | 0.0000707 |
| inclination: | 51.8965° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 304.9193° |
| argument of perigee: | 126.5752° |
| revolutions per day: | 14.79935746 |
| mean anomaly at epoch: | 233.5276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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