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 12078U 26150.44758762 +.00000000 +00000-0 +00000-0 0 00008
2 12078 73.3129 46.4838 4692238 302.9232 285.0340 2.00698304 07
| Epoch (UTC): | 30 May 2026 10:44:31 |
| Eccentricity: | 0.4692238 |
| inclination: | 73.3129° |
| perigee height: | 7713 km |
| apogee height: | 32628 km |
| right ascension of ascending node: | 46.4838° |
| argument of perigee: | 302.9232° |
| revolutions per day: | 2.00698304 |
| mean anomaly at epoch: | 285.0340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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