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 67721U 26145.11305025 +.00000000 +00000-0 +65718-3 0 00001
2 67721 97.2859 198.5710 0001080 85.6996 274.4370 15.33453372 01
| Epoch (UTC): | 25 May 2026 02:42:47 |
| Eccentricity: | 0.0001080 |
| inclination: | 97.2859° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.5710° |
| argument of perigee: | 85.6996° |
| revolutions per day: | 15.33453372 |
| mean anomaly at epoch: | 274.4370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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