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 64449U 26145.54936406 +.00000000 +00000-0 -22456-3 0 00008
2 64449 53.1597 91.3140 0001865 42.4207 317.6940 15.34434556 06
| Epoch (UTC): | 25 May 2026 13:11:05 |
| Eccentricity: | 0.0001865 |
| inclination: | 53.1597° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 91.3140° |
| argument of perigee: | 42.4207° |
| revolutions per day: | 15.34434556 |
| mean anomaly at epoch: | 317.6940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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