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 64821U 26145.62616663 +.00000000 +00000-0 +10639-2 0 00009
2 64821 51.8907 261.9939 0007740 300.5719 59.4522 15.80846051 00
| Epoch (UTC): | 25 May 2026 15:01:40 |
| Eccentricity: | 0.0007740 |
| inclination: | 51.8907° |
| perigee height: | 323 km |
| apogee height: | 333 km |
| right ascension of ascending node: | 261.9939° |
| argument of perigee: | 300.5719° |
| revolutions per day: | 15.80846051 |
| mean anomaly at epoch: | 59.4522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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