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 06061U 26088.15916091 +.00000000 +00000-0 +11035-3 0 00005
2 06061 74.0579 13.0426 0018281 57.3228 302.9688 14.42137122 03
| Epoch (UTC): | 29 March 2026 03:49:11 |
| Eccentricity: | 0.0018281 |
| inclination: | 74.0579° |
| perigee height: | 738 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 13.0426° |
| argument of perigee: | 57.3228° |
| revolutions per day: | 14.42137122 |
| mean anomaly at epoch: | 302.9688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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