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 12624U 26150.02036448 +.00000000 +00000-0 +44838-3 0 00009
2 12624 90.8980 47.5025 6246543 207.4646 97.3022 3.52917353 04
| Epoch (UTC): | 30 May 2026 00:29:19 |
| Eccentricity: | 0.6246543 |
| inclination: | 90.8980° |
| perigee height: | 462 km |
| apogee height: | 23228 km |
| right ascension of ascending node: | 47.5025° |
| argument of perigee: | 207.4646° |
| revolutions per day: | 3.52917353 |
| mean anomaly at epoch: | 97.3022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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