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 62753U 26145.51819852 +.00000000 +00000-0 +42734-3 0 00006
2 62753 42.9955 80.8167 0001252 281.5512 78.5199 15.27589964 08
| Epoch (UTC): | 25 May 2026 12:26:12 |
| Eccentricity: | 0.0001252 |
| inclination: | 42.9955° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.8167° |
| argument of perigee: | 281.5512° |
| revolutions per day: | 15.27589964 |
| mean anomaly at epoch: | 78.5199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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