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 38770U 26074.87772307 +.00000000 +00000-0 +10688-2 0 00003
2 38770 64.6194 204.9579 0018814 245.1154 114.8054 15.98725355 00
| Epoch (UTC): | 15 March 2026 21:03:55 |
| Eccentricity: | 0.0018814 |
| inclination: | 64.6194° |
| perigee height: | 265 km |
| apogee height: | 290 km |
| right ascension of ascending node: | 204.9579° |
| argument of perigee: | 245.1154° |
| revolutions per day: | 15.98725355 |
| mean anomaly at epoch: | 114.8054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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