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 67715U 26145.24303520 +.00000000 +00000-0 +11361-2 0 00000
2 67715 97.2832 256.8445 0001654 80.8106 279.3323 15.33451980 00
| Epoch (UTC): | 25 May 2026 05:49:58 |
| Eccentricity: | 0.0001654 |
| inclination: | 97.2832° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 256.8445° |
| argument of perigee: | 80.8106° |
| revolutions per day: | 15.33451980 |
| mean anomaly at epoch: | 279.3323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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