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 16262U 26064.16616726 +.00000000 +00000-0 +53212-3 0 00009
2 16262 82.4617 326.3549 0006646 30.9225 329.2416 15.50327167 06
| Epoch (UTC): | 05 March 2026 03:59:16 |
| Eccentricity: | 0.0006646 |
| inclination: | 82.4617° |
| perigee height: | 411 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 326.3549° |
| argument of perigee: | 30.9225° |
| revolutions per day: | 15.50327167 |
| mean anomaly at epoch: | 329.2416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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