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 26141.21778198 +.00000000 +00000-0 +58936-4 0 00006
2 37380 71.9715 205.6860 0014943 171.0065 189.1371 14.84595814 00
| Epoch (UTC): | 21 May 2026 05:13:36 |
| Eccentricity: | 0.0014943 |
| inclination: | 71.9715° |
| perigee height: | 604 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 205.6860° |
| argument of perigee: | 171.0065° |
| revolutions per day: | 14.84595814 |
| mean anomaly at epoch: | 189.1371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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