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 64695U 26088.20222670 +.00000000 +00000-0 +40563-3 0 00009
2 64695 98.0789 37.0796 0093154 88.4233 272.7653 14.90573033 02
| Epoch (UTC): | 29 March 2026 04:51:12 |
| Eccentricity: | 0.0093154 |
| inclination: | 98.0789° |
| perigee height: | 531 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 37.0796° |
| argument of perigee: | 88.4233° |
| revolutions per day: | 14.90573033 |
| mean anomaly at epoch: | 272.7653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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