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 07364U 26159.19764697 +.00000000 +00000-0 +60477-4 0 00003
2 07364 81.2319 213.3761 0048423 291.7069 67.8948 14.06460098 04
| Epoch (UTC): | 08 June 2026 04:44:36 |
| Eccentricity: | 0.0048423 |
| inclination: | 81.2319° |
| perigee height: | 836 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 213.3761° |
| argument of perigee: | 291.7069° |
| revolutions per day: | 14.06460098 |
| mean anomaly at epoch: | 67.8948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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