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 26044.70458256 +.00000000 +00000-0 +12191-3 0 00009
2 27421 98.0034 88.9442 0128579 300.8007 58.0586 14.54634291 08
| Epoch (UTC): | 13 February 2026 16:54:35 |
| Eccentricity: | 0.0128579 |
| inclination: | 98.0034° |
| perigee height: | 619 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 88.9442° |
| argument of perigee: | 300.8007° |
| revolutions per day: | 14.54634291 |
| mean anomaly at epoch: | 58.0586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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