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 03081U 26088.20355794 +.00000000 +00000-0 +41394-4 0 00009
2 03081 65.1414 130.9890 0013773 125.5103 234.7250 13.93388522 00
| Epoch (UTC): | 29 March 2026 04:53:07 |
| Eccentricity: | 0.0013773 |
| inclination: | 65.1414° |
| perigee height: | 907 km |
| apogee height: | 927 km |
| right ascension of ascending node: | 130.9890° |
| argument of perigee: | 125.5103° |
| revolutions per day: | 13.93388522 |
| mean anomaly at epoch: | 234.7250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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