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 62676U 26144.95281431 +.00000000 +00000-0 +11313-3 0 00002
2 62676 97.3959 223.6465 0006689 69.1018 291.0933 15.21009158 02
| Epoch (UTC): | 24 May 2026 22:52:03 |
| Eccentricity: | 0.0006689 |
| inclination: | 97.3959° |
| perigee height: | 498 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 223.6465° |
| argument of perigee: | 69.1018° |
| revolutions per day: | 15.21009158 |
| mean anomaly at epoch: | 291.0933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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