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 64749U 26145.38907785 +.00000000 +00000-0 +47056-3 0 00003
2 64749 53.1582 184.8608 0001020 85.1248 274.9869 15.30212960 06
| Epoch (UTC): | 25 May 2026 09:20:16 |
| Eccentricity: | 0.0001020 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.8608° |
| argument of perigee: | 85.1248° |
| revolutions per day: | 15.30212960 |
| mean anomaly at epoch: | 274.9869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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