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 22913U 26071.65776910 +.00000000 +00000-0 +14417-2 0 00006
2 22913 6.7337 137.5792 1595481 14.4761 349.6213 12.47369954 03
| Epoch (UTC): | 12 March 2026 15:47:11 |
| Eccentricity: | 0.1595481 |
| inclination: | 6.7337° |
| perigee height: | 222 km |
| apogee height: | 2729 km |
| right ascension of ascending node: | 137.5792° |
| argument of perigee: | 14.4761° |
| revolutions per day: | 12.47369954 |
| mean anomaly at epoch: | 349.6213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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