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 37380U 26150.85339336 +.00000000 +00000-0 +11405-3 0 00002
2 37380 71.9703 184.1728 0014291 152.2134 207.9798 14.84611625 06
| Epoch (UTC): | 30 May 2026 20:28:53 |
| Eccentricity: | 0.0014291 |
| inclination: | 71.9703° |
| perigee height: | 605 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 184.1728° |
| argument of perigee: | 152.2134° |
| revolutions per day: | 14.84611625 |
| mean anomaly at epoch: | 207.9798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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