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 63374U 26145.58335647 +.00000000 +00000-0 +17801-2 0 00004
2 63374 53.1607 52.6175 0001311 99.1663 126.3344 15.33495264 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001311 |
| inclination: | 53.1607° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 52.6175° |
| argument of perigee: | 99.1663° |
| revolutions per day: | 15.33495264 |
| mean anomaly at epoch: | 126.3344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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