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 39153U 26038.95075118 +.00000000 +00000-0 +46410-3 0 00007
2 39153 98.1466 193.3513 0011565 213.3450 146.7042 14.96278541 09
| Epoch (UTC): | 07 February 2026 22:49:04 |
| Eccentricity: | 0.0011565 |
| inclination: | 98.1466° |
| perigee height: | 570 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 193.3513° |
| argument of perigee: | 213.3450° |
| revolutions per day: | 14.96278541 |
| mean anomaly at epoch: | 146.7042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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