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 07298U 26106.76213677 +.00000000 +00000-0 +00000-0 0 00003
2 07298 4.2947 249.1141 0016671 76.5323 337.6847 0.98614890 06
| Epoch (UTC): | 16 April 2026 18:17:28 |
| Eccentricity: | 0.0016671 |
| inclination: | 4.2947° |
| perigee height: | 36187 km |
| apogee height: | 36329 km |
| right ascension of ascending node: | 249.1141° |
| argument of perigee: | 76.5323° |
| revolutions per day: | 0.98614890 |
| mean anomaly at epoch: | 337.6847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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