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 37677U 26145.45812021 +.00000000 +00000-0 +00000-0 0 00004
2 37677 0.9904 84.4401 0003208 341.7853 67.2467 1.00273141 00
| Epoch (UTC): | 25 May 2026 10:59:41 |
| Eccentricity: | 0.0003208 |
| inclination: | 0.9904° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 84.4401° |
| argument of perigee: | 341.7853° |
| revolutions per day: | 1.00273141 |
| mean anomaly at epoch: | 67.2467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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