▸Orbital parameters

Orbit class	SSO
Inclination	97.3771°
Eccentricity	0.0004188
Period	93.2 min
Apogee	432 km
Perigee	427 km
Mean motion	15.45698118 rev/day
RAAN	273.3050°
Arg of perigee	219.3554°
Mean anomaly	140.7391°
B*	5.2926e-4
Rev at epoch	10,538

▸Two-line element set (TLE)

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

1 60519U 24149BD 26187.23632372 .00025518 00000-0 52926-3 0 9991

2 60519 97.3771 273.3050 0004188 219.3554 140.7391 15.45698118105387

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FLOCK 4BE-28",
  "OBJECT_ID": "2024-149BD",
  "EPOCH": "2026-07-06T05:40:18.369+00:00",
  "MEAN_MOTION": 15.45698118,
  "ECCENTRICITY": 0.0004188,
  "INCLINATION": 97.3771,
  "RA_OF_ASC_NODE": 273.305,
  "ARG_OF_PERICENTER": 219.3554,
  "MEAN_ANOMALY": 140.7391,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60519,
  "REV_AT_EPOCH": 10538,
  "BSTAR": 0.00052926,
  "MEAN_MOTION_DOT": 0.00025518,
  "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-28
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/60519

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