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 37384U 26139.76799346 +.00000000 +00000-0 +00000-0 0 00000
2 37384 62.3699 40.4207 0033808 185.8234 35.8952 1.00273682 03
| Epoch (UTC): | 19 May 2026 18:25:54 |
| Eccentricity: | 0.0033808 |
| inclination: | 62.3699° |
| perigee height: | 35644 km |
| apogee height: | 35929 km |
| right ascension of ascending node: | 40.4207° |
| argument of perigee: | 185.8234° |
| revolutions per day: | 1.00273682 |
| mean anomaly at epoch: | 35.8952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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