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 26076.19082519 +.00000000 +00000-0 +87277-3 0 00008
2 38770 64.6197 200.1251 0018006 248.0752 111.8499 15.99992834 06
| Epoch (UTC): | 17 March 2026 04:34:47 |
| Eccentricity: | 0.0018006 |
| inclination: | 64.6197° |
| perigee height: | 262 km |
| apogee height: | 286 km |
| right ascension of ascending node: | 200.1251° |
| argument of perigee: | 248.0752° |
| revolutions per day: | 15.99992834 |
| mean anomaly at epoch: | 111.8499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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