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 26158.74996082 +.00000000 +00000-0 +70323-4 0 00006
2 21419 74.0402 60.8311 0041260 267.6318 92.0110 14.35273322 06
| Epoch (UTC): | 07 June 2026 17:59:56 |
| Eccentricity: | 0.0041260 |
| inclination: | 74.0402° |
| perigee height: | 745 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 60.8311° |
| argument of perigee: | 267.6318° |
| revolutions per day: | 14.35273322 |
| mean anomaly at epoch: | 92.0110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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