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 07715U 26088.19642191 +.00000000 +00000-0 +94926-4 0 00004
2 07715 81.2247 356.8261 0050282 108.5202 252.1440 14.07198451 00
| Epoch (UTC): | 29 March 2026 04:42:50 |
| Eccentricity: | 0.0050282 |
| inclination: | 81.2247° |
| perigee height: | 833 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 356.8261° |
| argument of perigee: | 108.5202° |
| revolutions per day: | 14.07198451 |
| mean anomaly at epoch: | 252.1440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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