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 26069.55164307 +.00000000 +00000-0 +12518-2 0 00001
2 38770 64.6211 224.4657 0022148 235.3842 124.5230 15.93535704 00
| Epoch (UTC): | 10 March 2026 13:14:21 |
| Eccentricity: | 0.0022148 |
| inclination: | 64.6211° |
| perigee height: | 278 km |
| apogee height: | 307 km |
| right ascension of ascending node: | 224.4657° |
| argument of perigee: | 235.3842° |
| revolutions per day: | 15.93535704 |
| mean anomaly at epoch: | 124.5230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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