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 64440U 26145.54567959 +.00000000 +00000-0 +61939-3 0 00000
2 64440 53.1582 91.2959 0001243 95.3172 264.7971 15.30228072 02
| Epoch (UTC): | 25 May 2026 13:05:46 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.2959° |
| argument of perigee: | 95.3172° |
| revolutions per day: | 15.30228072 |
| mean anomaly at epoch: | 264.7971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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