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 64898U 26145.63689817 +.00000000 +00000-0 +51345-3 0 00005
2 64898 97.6679 210.2612 0003675 343.8767 16.2337 14.95913363 00
| Epoch (UTC): | 25 May 2026 15:17:08 |
| Eccentricity: | 0.0003675 |
| inclination: | 97.6679° |
| perigee height: | 577 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 210.2612° |
| argument of perigee: | 343.8767° |
| revolutions per day: | 14.95913363 |
| mean anomaly at epoch: | 16.2337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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