▸Orbital parameters

Orbit class	SSO
Inclination	97.7223°
Eccentricity	0.0004458
Period	95.7 min
Apogee	557 km
Perigee	551 km
Mean motion	15.04138808 rev/day
RAAN	270.8397°
Arg of perigee	82.7690°
Mean anomaly	277.4043°
B*	4.8362e-4
Rev at epoch	8,063

▸Two-line element set (TLE)

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

1 62711U 25009DG 26188.18676830 .00006648 00000-0 48362-3 0 9997

2 62711 97.7223 270.8397 0004458 82.7690 277.4043 15.04138808 80630

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-ROUNDTRIPPER",
  "OBJECT_ID": "2025-009DG",
  "EPOCH": "2026-07-07T04:28:56.781+00:00",
  "MEAN_MOTION": 15.04138808,
  "ECCENTRICITY": 0.0004458,
  "INCLINATION": 97.7223,
  "RA_OF_ASC_NODE": 270.8397,
  "ARG_OF_PERICENTER": 82.769,
  "MEAN_ANOMALY": 277.4043,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62711,
  "REV_AT_EPOCH": 8063,
  "BSTAR": 0.00048362,
  "MEAN_MOTION_DOT": 0.00006648,
  "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	LEMUR-2-ROUNDTRIPPER
Operator	SpireHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 14, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	7.6HIGHvia 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/62711

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