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 27421U 26150.08188380 +.00000000 +00000-0 +99132-4 0 00007
2 27421 97.9857 189.7455 0128928 333.3353 26.1252 14.54737262 04
| Epoch (UTC): | 30 May 2026 01:57:54 |
| Eccentricity: | 0.0128928 |
| inclination: | 97.9857° |
| perigee height: | 619 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 189.7455° |
| argument of perigee: | 333.3353° |
| revolutions per day: | 14.54737262 |
| mean anomaly at epoch: | 26.1252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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