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 64199U 26145.14265524 +.00000000 +00000-0 +19781-3 0 00008
2 64199 97.4556 223.8208 0020654 75.6417 284.7111 15.23404275 06
| Epoch (UTC): | 25 May 2026 03:25:25 |
| Eccentricity: | 0.0020654 |
| inclination: | 97.4556° |
| perigee height: | 481 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 223.8208° |
| argument of perigee: | 75.6417° |
| revolutions per day: | 15.23404275 |
| mean anomaly at epoch: | 284.7111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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