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 26150.28389958 +.00000000 +00000-0 +00000-0 0 00008
2 02412 90.3351 277.0217 0007312 86.0359 274.1328 8.59079282 09
| Epoch (UTC): | 30 May 2026 06:48:48 |
| Eccentricity: | 0.0007312 |
| inclination: | 90.3351° |
| perigee height: | 3685 km |
| apogee height: | 3700 km |
| right ascension of ascending node: | 277.0217° |
| argument of perigee: | 86.0359° |
| revolutions per day: | 8.59079282 |
| mean anomaly at epoch: | 274.1328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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