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 64903U 26145.57737383 +.00000000 +00000-0 +21353-3 0 00003
2 64903 97.4329 224.4948 0000923 129.1930 230.9387 15.20196856 05
| Epoch (UTC): | 25 May 2026 13:51:25 |
| Eccentricity: | 0.0000923 |
| inclination: | 97.4329° |
| perigee height: | 505 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 224.4948° |
| argument of perigee: | 129.1930° |
| revolutions per day: | 15.20196856 |
| mean anomaly at epoch: | 230.9387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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