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 45374U 26145.44153567 +.00000000 +00000-0 +92084-3 0 00005
2 45374 53.1580 168.1199 0004752 39.4035 320.7313 15.33997683 07
| Epoch (UTC): | 25 May 2026 10:35:48 |
| Eccentricity: | 0.0004752 |
| inclination: | 53.1580° |
| perigee height: | 461 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 168.1199° |
| argument of perigee: | 39.4035° |
| revolutions per day: | 15.33997683 |
| mean anomaly at epoch: | 320.7313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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