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 02412U 26087.98763977 +.00000000 +00000-0 +00000-0 0 00001
2 02412 90.3262 276.3054 0007145 144.0254 216.1079 8.59079549 09
| Epoch (UTC): | 28 March 2026 23:42:12 |
| Eccentricity: | 0.0007145 |
| inclination: | 90.3262° |
| perigee height: | 3685 km |
| apogee height: | 3699 km |
| right ascension of ascending node: | 276.3054° |
| argument of perigee: | 144.0254° |
| revolutions per day: | 8.59079549 |
| mean anomaly at epoch: | 216.1079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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