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 12376U 26150.10922553 +.00000000 +00000-0 +00000-0 0 00003
2 12376 68.8652 90.5262 5864862 351.1156 1.7510 2.00768674 05
| Epoch (UTC): | 30 May 2026 02:37:17 |
| Eccentricity: | 0.5864862 |
| inclination: | 68.8652° |
| perigee height: | 4597 km |
| apogee height: | 35731 km |
| right ascension of ascending node: | 90.5262° |
| argument of perigee: | 351.1156° |
| revolutions per day: | 2.00768674 |
| mean anomaly at epoch: | 1.7510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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