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 21055U 26150.61888883 +.00000000 +00000-0 +00000-0 0 00000
2 21055 14.5536 351.6398 0014290 52.1311 303.7639 0.99956546 07
| Epoch (UTC): | 30 May 2026 14:51:11 |
| Eccentricity: | 0.0014290 |
| inclination: | 14.5536° |
| perigee height: | 35815 km |
| apogee height: | 35936 km |
| right ascension of ascending node: | 351.6398° |
| argument of perigee: | 52.1311° |
| revolutions per day: | 0.99956546 |
| mean anomaly at epoch: | 303.7639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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