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 21419U 26161.39860478 +.00000000 +00000-0 +52862-4 0 00008
2 21419 74.0402 55.9755 0041230 262.3076 97.3393 14.35274140 03
| Epoch (UTC): | 10 June 2026 09:33:59 |
| Eccentricity: | 0.0041230 |
| inclination: | 74.0402° |
| perigee height: | 745 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 55.9755° |
| argument of perigee: | 262.3076° |
| revolutions per day: | 14.35274140 |
| mean anomaly at epoch: | 97.3393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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