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 10974U 26088.21151838 +.00000000 +00000-0 +70875-4 0 00008
2 10974 82.4848 8.4817 0017382 140.3519 219.8975 14.90032369 07
| Epoch (UTC): | 29 March 2026 05:04:35 |
| Eccentricity: | 0.0017382 |
| inclination: | 82.4848° |
| perigee height: | 586 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 8.4817° |
| argument of perigee: | 140.3519° |
| revolutions per day: | 14.90032369 |
| mean anomaly at epoch: | 219.8975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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