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 26071.76377519 +.00000000 +00000-0 +61319-4 0 00008
2 07210 81.2389 162.6996 0079432 302.8591 56.4953 14.13625256 02
| Epoch (UTC): | 12 March 2026 18:19:50 |
| Eccentricity: | 0.0079432 |
| inclination: | 81.2389° |
| perigee height: | 790 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 162.6996° |
| argument of perigee: | 302.8591° |
| revolutions per day: | 14.13625256 |
| mean anomaly at epoch: | 56.4953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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