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 40012U 26138.41366947 +.00000000 +00000-0 +20500-3 0 00000
2 40012 97.7845 291.6603 0045647 164.9975 195.2608 14.88053881 00
| Epoch (UTC): | 18 May 2026 09:55:41 |
| Eccentricity: | 0.0045647 |
| inclination: | 97.7845° |
| perigee height: | 572 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 291.6603° |
| argument of perigee: | 164.9975° |
| revolutions per day: | 14.88053881 |
| mean anomaly at epoch: | 195.2608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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