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 12472U 26106.13150875 +.00000000 +00000-0 +00000-0 0 00004
2 12472 9.4704 316.0822 0003875 345.3434 211.6861 1.00205488 06
| Epoch (UTC): | 16 April 2026 03:09:22 |
| Eccentricity: | 0.0003875 |
| inclination: | 9.4704° |
| perigee height: | 35789 km |
| apogee height: | 35822 km |
| right ascension of ascending node: | 316.0822° |
| argument of perigee: | 345.3434° |
| revolutions per day: | 1.00205488 |
| mean anomaly at epoch: | 211.6861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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