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 64759U 26145.54734270 +.00000000 +00000-0 +12042-2 0 00005
2 64759 53.1599 245.4245 0002534 56.7527 303.3718 15.33626753 03
| Epoch (UTC): | 25 May 2026 13:08:10 |
| Eccentricity: | 0.0002534 |
| inclination: | 53.1599° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 245.4245° |
| argument of perigee: | 56.7527° |
| revolutions per day: | 15.33626753 |
| mean anomaly at epoch: | 303.3718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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