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 07210U 26064.26116625 +.00000000 +00000-0 +10961-3 0 00000
2 07210 81.2389 170.0498 0079630 324.3994 35.1881 14.13622211 00
| Epoch (UTC): | 05 March 2026 06:16:04 |
| Eccentricity: | 0.0079630 |
| inclination: | 81.2389° |
| perigee height: | 789 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 170.0498° |
| argument of perigee: | 324.3994° |
| revolutions per day: | 14.13622211 |
| mean anomaly at epoch: | 35.1881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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