▸Orbital parameters

Orbit class	SSO
Inclination	97.3790°
Eccentricity	0.0003132
Period	93.5 min
Apogee	450 km
Perigee	446 km
Mean motion	15.39388814 rev/day
RAAN	271.4701°
Arg of perigee	160.0470°
Mean anomaly	200.0899°
B*	2.7493e-4
Rev at epoch	10,531

▸Two-line element set (TLE)

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

1 60487U 24149V 26188.17767941 .00010672 00000-0 27493-3 0 9996

2 60487 97.3790 271.4701 0003132 160.0470 200.0899 15.39388814105319

▸ source OMM (JSON)

{
  "OBJECT_NAME": "FLOCK 4BE-25",
  "OBJECT_ID": "2024-149V",
  "EPOCH": "2026-07-07T04:15:51.501+00:00",
  "MEAN_MOTION": 15.39388814,
  "ECCENTRICITY": 0.0003132,
  "INCLINATION": 97.379,
  "RA_OF_ASC_NODE": 271.4701,
  "ARG_OF_PERICENTER": 160.047,
  "MEAN_ANOMALY": 200.0899,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60487,
  "REV_AT_EPOCH": 10531,
  "BSTAR": 0.00027493,
  "MEAN_MOTION_DOT": 0.00010672,
  "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-25
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/60487

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