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 52787U 26088.15608612 +.00000000 +00000-0 +43448-3 0 00001
2 52787 49.9859 210.9622 0008597 160.6307 199.4958 14.81106778 07
| Epoch (UTC): | 29 March 2026 03:44:45 |
| Eccentricity: | 0.0008597 |
| inclination: | 49.9859° |
| perigee height: | 620 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 210.9622° |
| argument of perigee: | 160.6307° |
| revolutions per day: | 14.81106778 |
| mean anomaly at epoch: | 199.4958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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