▸Orbital parameters

Orbit class	SSO
Inclination	97.3835°
Eccentricity	0.0003199
Period	93.5 min
Apogee	446 km
Perigee	441 km
Mean motion	15.40868016 rev/day
RAAN	271.9030°
Arg of perigee	198.4527°
Mean anomaly	161.6603°
B*	3.4189e-4
Rev at epoch	10,528

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 60559U 24149CV 26187.70827036 .00013961 00000-0 34189-3 0 9990

2 60559 97.3835 271.9030 0003199 198.4527 161.6603 15.40868016105280

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FLOCK 4BE-5",
  "OBJECT_ID": "2024-149CV",
  "EPOCH": "2026-07-06T16:59:54.559+00:00",
  "MEAN_MOTION": 15.40868016,
  "ECCENTRICITY": 0.0003199,
  "INCLINATION": 97.3835,
  "RA_OF_ASC_NODE": 271.903,
  "ARG_OF_PERICENTER": 198.4527,
  "MEAN_ANOMALY": 161.6603,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60559,
  "REV_AT_EPOCH": 10528,
  "BSTAR": 0.00034189,
  "MEAN_MOTION_DOT": 0.00013961,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	FLOCK 4BE-5
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5.7HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/60559

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.