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 64879U 26145.61687664 +.00000000 +00000-0 +33622-3 0 00008
2 64879 97.4540 114.0915 0005646 252.3620 107.7004 15.29658086 06
| Epoch (UTC): | 25 May 2026 14:48:18 |
| Eccentricity: | 0.0005646 |
| inclination: | 97.4540° |
| perigee height: | 473 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 114.0915° |
| argument of perigee: | 252.3620° |
| revolutions per day: | 15.29658086 |
| mean anomaly at epoch: | 107.7004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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