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 07364U 26088.05748927 +.00000000 +00000-0 +59933-4 0 00002
2 07364 81.2282 282.3129 0049849 130.9961 229.5536 14.06447175 06
| Epoch (UTC): | 29 March 2026 01:22:47 |
| Eccentricity: | 0.0049849 |
| inclination: | 81.2282° |
| perigee height: | 835 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 282.3129° |
| argument of perigee: | 130.9961° |
| revolutions per day: | 14.06447175 |
| mean anomaly at epoch: | 229.5536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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