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 26067.13504821 +.00000000 +00000-0 +65786-3 0 00000
2 16262 82.4605 323.2481 0006138 22.1093 338.0422 15.50520669 03
| Epoch (UTC): | 08 March 2026 03:14:28 |
| Eccentricity: | 0.0006138 |
| inclination: | 82.4605° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 323.2481° |
| argument of perigee: | 22.1093° |
| revolutions per day: | 15.50520669 |
| mean anomaly at epoch: | 338.0422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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