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 49330U 26145.80055919 +.00000000 +00000-0 +00000-0 0 00007
2 49330 5.0624 61.3152 0048118 168.7763 69.2025 1.00263970 08
| Epoch (UTC): | 25 May 2026 19:12:48 |
| Eccentricity: | 0.0048118 |
| inclination: | 5.0624° |
| perigee height: | 35586 km |
| apogee height: | 35992 km |
| right ascension of ascending node: | 61.3152° |
| argument of perigee: | 168.7763° |
| revolutions per day: | 1.00263970 |
| mean anomaly at epoch: | 69.2025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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